Rotor hub assembly with universal joint

ABSTRACT

A rotor hub assembly that includes a yoke configured to attach blades thereto, a universal joint configured to attach to, and transmit forces between, a mast and the yoke, and an elastomeric member configured to attenuate vibrations transmitted from the universal joint to the mast.

CROSS-REFERENCE TO RELATED APPLICATIONS

This is a divisional application of application Ser. No. 15/658,190,which was filed on 24 Jul. 2017 and entitled “Rotor Hub Assembly withUniversal Joint,” the entire content of which is hereby expresslyincorporated by reference.

BACKGROUND

Rotorcraft often utilize a gimbaled drive joint to allow the axis ofrotation of the rotor hub to vary relative to the mast axis. Thesegimbaled drive joints may utilize universal joints (also known as aHooke's joint or a Cardin joint) to accomplish the variable axis ofrotation. However, the universal joints produce an undesirable two perrevolution (“2/rev”) torsional drive force. In the past, two-bladedhelicopters dealt with these torsional 2/rev forces that originate inthe gimbaled hub flapping joint by tuning the drive train to avoid 2/revresonances by using long slender masts that were torsionally soft. Theselong, thin, torsionally soft masts would attenuate the vibration. Thelong torsionally soft mast and careful tuning of all the drive elementsof the rotor drive train have been used to produce helicopters that canrun for thousands of hours with no issues from the torsional 2/revforces and motions that are inherent in two-bladed rotor systems.However, tiltrotor aircraft require very stiff hubs in the chord wisedirection and very stiff masts, pylons, and wings to prevent whirlflutter instability problems in the rotor system during high speedairplane flight. As such, the ability to attenuate the 2/rev vibrationvia long torsionally soft masts is not possible in tiltrotor aircraft.In a prior tiltrotor aircraft, it was attempted to solve the 2/revdilemma by utilizing a true constant velocity joint instead of a simpleruniversal joint. However, even the true constant velocity joint producedunwanted 2/rev vibrations. In order to reduce the overall rotor hub2/rev vibrations to a tolerable level, a pair of very heavy pendulumassemblies and additional vibration treatment were required. As such,there is a need to develop a simple, lightweight, gimbaled rotor hubassembly that will attenuate the 2/rev vibrations.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is an oblique view of a rotor hub assembly according to thisdisclosure.

FIG. 2 is an oblique view of the rotor hub assembly of FIG. 1.

FIG. 3 is an oblique view of a portion of the rotor hub assembly ofFIGS. 1 and 2.

FIG. 4 is an oblique view of a portion of the rotor hub assembly ofFIGS. 1-3.

FIG. 5 is an exploded view of a portion of the rotor hub assembly ofFIGS. 1-4.

FIG. 6 is an oblique view of an elastomeric member of the rotor hubassembly of FIGS. 1-5.

FIG. 7 is an oblique view of another rotor hub assembly according tothis disclosure.

FIG. 8 is an exploded view of the rotor hub assembly of FIG. 7.

FIG. 9 is an oblique view of a portion of the rotor mast assembly ofFIGS. 7 and 8.

DETAILED DESCRIPTION

In this disclosure, reference may be made to the spatial relationshipsbetween various components and to the spatial orientation of variousaspects of components as the devices are depicted in the attacheddrawings. However, as will be recognized by those skilled in the artafter a complete reading of this disclosure, the devices, members,apparatuses, etc. described herein may be positioned in any desiredorientation. Thus, the use of terms such as “above,” “below,” “upper,”“lower,” or other like terms to describe a spatial relationship betweenvarious components or to describe the spatial orientation of aspects ofsuch components should be understood to describe a relative relationshipbetween the components or a spatial orientation of aspects of suchcomponents, respectively, as the device described herein may be orientedin any desired direction.

The solution presented in this disclosure solves the dilemma of 2/revvibrations in a gimbaled rotor hub by using a rotor hub assembly with auniversal joint and an elastomeric mast joint that may be used to tunethe natural frequency away from the 2/rev torsional oscillatory driveforces that are generated by the universal joint. This simplifiedsolution will not only save money but will also save a substantialamount of weight. While the disclosed rotor hub assembly may be used onany rotorcraft, it is particularly well-suited for use on tiltrotoraircraft.

As shown in FIGS. 1 and 2, a rotor hub assembly 101 is illustrated.Rotor hub assembly 101 is shown optionally disposed within a shroud 103(shown cut-away). Rotor hub assembly 101 is attached to a rotor mast 105to facilitate the transmission of torque from a powerplant to cause therotation of blades 107, thereby generating lift and/or thrust. Rotor hubassembly 101 includes a universal joint 109 attached to a yoke 111.Universal joint 109 permits yoke 111 to rotate about an axis of rotationthat is free to move relative to the axis of rotation of rotor mast 105.Yoke 111 includes four arms 113 extending therefrom to support blades107. As shown, arms 113 may include structure to facilitate theattachment of outboard shear/CF bearings 115 as well as inboard pitchbearings 117.

FIG. 3 illustrates universal joint 109 attached to rotor mast 105.Universal joint 109 includes a pair of yoke brackets 119A, 119B. Whileyoke brackets 119A, 119B are shown as a pair, it should be understoodthat yoke brackets 119A, 119B could be one unitary yoke bracket. Eachyoke bracket 119A, 119B includes a base 121A, 121B for providing astable connection with yoke 111. Bases 121A, 121B include a plurality ofopenings 123A, 123B extending therethrough to accept hardware forattaching yoke brackets 119A, 119B to yoke 111. Extending from bases121A, 121B are tabs 125A, 125B. Tabs 125A, 125B define openings 127A,127B extending therethrough. Opening 127A and opening 127B are coaxialalong a central longitudinal axis 129. Each opening 127A, 127B isconfigured to receive a hinge pin 131A, 131B and a radial bearing 133A,133B therein. Hinge pins 131A, 131B connect yoke brackets 119A, 119B toa cross member 135 via a first aperture 137 and a second aperture 139.First aperture 137 and second aperture 139 are also coaxial aboutcentral longitudinal axis 129. Hinge pin 131A extends from opening 127Ato first aperture 137. First aperture 137 may also include a radialbearing 141 configured to facilitate rotation of hinge pin 131A therein.Similarly, second aperture 139 may include a radial bearing 143configured to facilitate rotation of hinge pin 131B therein. Universaljoint 109 also includes a drive member 145 configured to transfer torquefrom rotor mast 105 to cross member 135.

Referring to FIGS. 4 and 5, drive member 145 is shown in more detail.Drive member 145 includes an inner member 147 having an inner surface149 configured to engage rotor mast 105. This engagement may beaccomplished via the use of splines 151 on inner surface 149 andcomplementary splines 153 on rotor mast 105. Inner member 147 has anouter surface 155 that includes a plurality of projections 157 extendingtherefrom. Drive member 145 also includes an outer member 159surrounding inner member 147. Outer member 159 includes an inner surface161 that includes a plurality of projections 163 extending therefrom,such that projections 163 interlace with projections 157. A plurality ofelastomeric members 165 are disposed between the interlaced projections157 and 163. Outer member 159 also includes an outer surface 167 with apair of trunnions 169A, 169B extending therefrom. As shown in FIG. 3,trunnion 169A extends into a third aperture 171 of cross member 135, andtrunnion 169B extends in a fourth aperture 173 of cross member 135,wherein third aperture 171 and fourth aperture 173 are coaxial aboutcentral longitudinal axis 175. Accordingly, cross member 135 ispivotally attached to drive member 145 about central longitudinal axis175.

As shown in FIG. 6, elastomeric members 165 may be made of alternatinglayers of elastomeric material 177 and rigid material 179. Elastomericmaterial 177 may comprise natural or synthetic rubber, or any otherelastomeric material suitable for such application. Rigid material 179may be formed of metal, plastic, composite, or any other materialsuitable for such application.

In operation, torque is transmitted through rotor mast 105 to drivemember 145, cross member 135, yoke brackets 119A, 119B, and yoke 111,which rotates blades 107. When yoke 111 rotates about an axis that isnot coincident with the axis of rotation of rotor mast 105, 2/revoscillations are generated by universal joint 109. These 2/revoscillations are attenuated by tuning elastomeric members 165 to absorbthem in compression, rather than allowing the oscillations to betransmitted down rotor mast 105 to the drivetrain.

Referring to FIGS. 7 and 8, a rotor hub assembly 201 is illustrated.Rotor hub assembly 201 is attached to a rotor mast 205 to facilitate thetransmission of torque from a powerplant to cause the rotation of blades(not shown), thereby generating lift and/or thrust. Rotor hub assembly201 includes a universal joint 209 attached to a yoke 211. Universaljoint 209 permits yoke 211 to rotate about an axis of rotation that isfree to move relative to the axis of rotation of rotor mast 205. Yoke211 includes three arms 213 extending therefrom to support the blades.Universal joint 209 includes a yoke bracket 219. Yoke bracket 219includes a base 221 for providing a stable connection with yoke 211.Base 221 includes a plurality of openings 223 extending therethrough toaccept hardware for attaching yoke bracket 219 to yoke 211. Extendingfrom base 221 are tabs 225A, 225B, 225C, 225D. Tabs 225A, 225B, 225C,225D define openings 227A, 227B, 227C, 227D extending therethrough,respectively. Openings 227A, 227B, 227C, 227D are coaxial along acentral longitudinal axis 229. Openings 227A and 227B are configured toreceive a hinge pin 231A and a radial bearing 233A therein. And openings227C and 227D are configured to receive a hinge pin 231B and a radialbearing 233B therein. Hinge pins 231A, 231B connect yoke bracket 219 toa cross member 235 via a first aperture 237 and a second aperture 239.First aperture 237 and second aperture 239 are also coaxial aboutcentral longitudinal axis 229. Hinge pin 231A extends from opening 227Athrough first aperture 237 to opening 227B. Hinge pin 231B extends fromopening 227C through second aperture 239 to opening 227D. Universaljoint 209 also includes a drive member 245 configured to transfer torquefrom rotor mast 205 to cross member 235.

Referring to FIGS. 8 and 9, drive member 245 includes an inner member247 having an inner surface 249 configured to engage rotor mast 205.Inner member 247 has a substantially cylindrical outer surface 255.Inner member 247 also includes a flange 256 extending radiallytherefrom. Flange 256 defines a plurality of openings 258 extendingtherethrough. Drive member 245 also includes an outer member 259surrounding inner member 247. Outer member 259 includes a substantiallycylindrical inner surface 261. Outer member 259 also includes a flange262 extending radially therefrom. Flange 262 includes a plurality ofopenings 264 extending therethrough. An elastomeric member 265 islocated between inner member 247 and outer member 259. The elastomericmember 265 includes a hollow cylindrical portion 266 configured to fitbetween substantially cylindrical outer surface 255 of inner member 247and substantially cylindrical inner surface 261 of outer member 259.Elastomeric member 265 includes a flange 268 extending therefrom. Flange268 includes a plurality of openings 270 extending therethrough. Outermember 259 also includes an outer surface 267 with a pair of trunnions269A, 269B extending therefrom. Trunnion 269A extends into a thirdaperture 271 of cross member 235, and trunnion 269B extends in a fourthaperture 273 of cross member 235, wherein third aperture 271 and fourthaperture 273 are coaxial about a central longitudinal axis 275.Accordingly, cross member 235 is pivotally attached to drive member 245about central longitudinal axis 275.

Drive member 245 may also include an elastomeric ring 281 and aninelastic ring 283. Elastomeric ring 281 and inelastic ring 283 eachinclude a plurality of openings extending therethrough, 285 and 287,respectively. When assembled, flange 262 of outer member 259 has flange268 of elastomeric member 265 on top thereof, followed by flange 256 ofinner member 247, then elastomeric ring 281, and finally inelastic ring283 on the top. Flanges 262, 268, 256 and rings 281, 283 are alignedsuch that openings 264, 270, 258, 285, 287 are aligned and receiveconnection bolts 289 therethrough.

In operation, torque is transmitted through rotor mast 205, drive member245, cross member 235, yoke bracket 219, and yoke 211, to rotate theblades. When yoke 211 rotates about an axis that is not coincident withthe axis of rotation of rotor mast 205, 2/rev oscillations are generatedby universal joint 209. These 2/rev oscillations are attenuated bytuning elastomeric member 265 and elastomeric ring 281 to absorb them inshear, rather than allowing the oscillations to be transmitted downrotor mast 205 to the drivetrain. Additional elastomeric rings 281 andinelastic rings 283 may be added as required.

In the embodiments shown, the drive members and cross members show themasts passing through the centers thereof. It should be understood thatthe drive member could be mounted to a distal end of the mast. Inaddition, axis about which the cross member is pivotally attached to theyoke bracket could be above or below the drive member.

At least one embodiment is disclosed, and variations, combinations,and/or modifications of the embodiment(s) and/or features of theembodiment(s) made by a person having ordinary skill in the art arewithin the scope of the disclosure. Alternative embodiments that resultfrom combining, integrating, and/or omitting features of theembodiment(s) are also within the scope of the disclosure. Wherenumerical ranges or limitations are expressly stated, such expressranges or limitations should be understood to include iterative rangesor limitations of like magnitude falling within the expressly statedranges or limitations (e.g., from about 1 to about 10 includes, 2, 3, 4,etc.; greater than 0.10 includes 0.11, 0.12, 0.13, etc.). For example,whenever a numerical range with a lower limit, RI, and an upper limit,R_(u), is disclosed, any number falling within the range is specificallydisclosed. In particular, the following numbers within the range arespecifically disclosed: R=R_(l)+k*(R_(u)−R_(l)), wherein k is a variableranging from 1 percent to 100 percent with a 1 percent increment, i.e.,k is 1 percent, 2 percent, 3 percent, 4 percent, 5 percent, . . . 50percent, 51 percent, 52 percent, . . . , 95 percent, 96 percent, 95percent, 98 percent, 99 percent, or 100 percent. Moreover, any numericalrange defined by two R numbers as defined in the above is alsospecifically disclosed. Use of the term “optionally” with respect to anyelement of a claim means that the element is required, or alternatively,the element is not required, both alternatives being within the scope ofthe claim. Use of broader terms such as comprises, includes, and havingshould be understood to provide support for narrower terms such asconsisting of, consisting essentially of, and comprised substantiallyof. Accordingly, the scope of protection is not limited by thedescription set out above but is defined by the claims that follow, thatscope including all equivalents of the subject matter of the claims.Each and every claim is incorporated as further disclosure into thespecification and the claims are embodiment(s) of the present invention.Also, the phrases “at least one of A, B, and C” and “A and/or B and/orC” should each be interpreted to include only A, only B, only C, or anycombination of A, B, and C.

What is claimed is:
 1. A rotor hub assembly, comprising: a yoke havingat least two arms extending therefrom; a yoke bracket attached to theyoke; a cross member defining a first aperture with a first centrallongitudinal axis and a second aperture with a second centrallongitudinal axis, the first central longitudinal axis being orthogonalto the second central longitudinal axis, the cross member beingpivotally attached to the yoke bracket about the first centrallongitudinal axis; and a drive member, comprising: an inner memberconfigured to engage a mast; an outer member pivotally attached to thecross member about the second central longitudinal axis; and anelastomeric member disposed between the inner member and the outermember; wherein the inner member has a substantially cylindrical outersurface, the outer member has a substantially cylindrical inner surface,and the elastomeric member includes a hollow cylindrical portionconfigured to fit between the substantially cylindrical outer surface ofthe inner member and the substantially cylindrical outer surface of theouter member.
 2. The rotor hub assembly of claim 1, wherein the crossmember further includes a third aperture coaxial with the first apertureand a fourth aperture coaxial with the second aperture.
 3. The rotor hubassembly of claim 1, wherein the first and second central longitudinalaxes are coplanar.
 4. The rotor hub assembly of claim 1, the elastomericmember being configured to attenuate 2/rev vibrations transmitted to theinner member from the outer member.
 5. The rotor hub assembly of claim1, wherein each of the inner member and outer member comprises a flangeextending therefrom, the flanges being coupled to each other.
 6. Therotor hub assembly of claim 5, wherein the elastomeric member comprisesa flange extending therefrom, the flange of the elastomeric member beingcoupled between the flanges of the inner and outer members.
 7. The rotorhub assembly of claim 5, wherein the flanges are coupled to each otherwith fasteners extending through the flanges.
 8. A rotor hub assembly,comprising: a yoke having at least two arms extending therefrom; a yokebracket attached to the yoke; a cross member defining a first aperturewith a first central longitudinal axis and a second aperture with asecond central longitudinal axis, the first central longitudinal axisbeing orthogonal to the second central longitudinal axis, the crossmember being pivotally attached to the yoke bracket about the firstcentral longitudinal axis; and a drive member, comprising: an innermember configured to engage a mast; an outer member pivotally attachedto the cross member about the second central longitudinal axis; and anelastomeric member disposed between the inner member and the outermember; wherein each of the inner member and outer member comprises aflange extending therefrom, the flanges being coupled to each other. 9.The rotor hub assembly of claim 8, wherein the cross member furtherincludes a third aperture coaxial with the first aperture and a fourthaperture coaxial with the second aperture.
 10. The rotor hub assembly ofclaim 8, wherein the first and second central longitudinal axes arecoplanar.
 11. The rotor hub assembly of claim 8, the elastomeric memberbeing configured to attenuate 2/rev vibrations transmitted to the innermember from the outer member.
 12. The rotor hub assembly of claim 8,wherein the inner member has a substantially cylindrical outer surface,the outer member has a substantially cylindrical inner surface, and theelastomeric member includes a hollow cylindrical portion configured tofit between the substantially cylindrical outer surface of the innermember and the substantially cylindrical outer surface of the outermember.
 13. The rotor hub assembly of claim 8, wherein the elastomericmember comprises a flange extending therefrom, the flange of theelastomeric member being coupled between the flanges of the inner andouter members.
 14. The rotor hub assembly of claim 8, wherein theflanges are coupled to each other with fasteners extending through theflanges.
 15. A rotor hub assembly, comprising: a yoke having at leasttwo arms extending therefrom; a yoke bracket attached to the yoke; across member defining a first aperture with a first central longitudinalaxis and a second aperture with a second central longitudinal axis, thefirst central longitudinal axis being orthogonal to the second centrallongitudinal axis, the cross member being pivotally attached to the yokebracket about the first central longitudinal axis; and a drive member,comprising: an inner member configured to engage a mast; an outer memberpivotally attached to the cross member about the second centrallongitudinal axis; and an elastomeric member disposed between the innermember and the outer member; wherein each of the inner member, outermember, and elastomeric member comprises a flange extending therefrom,the flanges of the inner and outer members being coupled to each other,and the flange of the elastomeric member being coupled between theflanges of the inner and outer members.
 16. The rotor hub assembly ofclaim 15, wherein the cross member further includes a third aperturecoaxial with the first aperture and a fourth aperture coaxial with thesecond aperture.
 17. The rotor hub assembly of claim 15, wherein thefirst and second central longitudinal axes are coplanar.
 18. The rotorhub assembly of claim 15, the elastomeric member being configured toattenuate 2/rev vibrations transmitted to the inner member from theouter member.
 19. The rotor hub assembly of claim 15, wherein the innermember has a substantially cylindrical outer surface, the outer memberhas a substantially cylindrical inner surface, and the elastomericmember includes a hollow cylindrical portion configured to fit betweenthe substantially cylindrical outer surface of the inner member and thesubstantially cylindrical outer surface of the outer member.